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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2009
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Article
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Fig 4
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Research Article
Controlling the Eccentricity of Polar Lunar Orbits with Low-Thrust Propulsion
Figure 4
Temporal evolution of the eccentricity (a) and of the orbital radius (b). In this simulation the initial altitude was 500 km and the thrust value used was 0.2 N.
(a)
(b)